DE1667252C - Rotary flow vortex for mass and heat exchange between solid or liquid particles and gases - Google Patents
Rotary flow vortex for mass and heat exchange between solid or liquid particles and gasesInfo
- Publication number
- DE1667252C DE1667252C DE1667252C DE 1667252 C DE1667252 C DE 1667252C DE 1667252 C DE1667252 C DE 1667252C
- Authority
- DE
- Germany
- Prior art keywords
- vortex
- particles
- inlet
- vortex chamber
- roughness
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 239000002245 particle Substances 0.000 title claims description 24
- 239000007789 gas Substances 0.000 title claims 15
- 239000007788 liquid Substances 0.000 title claims 7
- 239000007787 solid Substances 0.000 title claims 6
- 235000019592 roughness Nutrition 0.000 claims description 13
- 238000006243 chemical reaction Methods 0.000 claims description 4
- 238000001816 cooling Methods 0.000 claims description 3
- 239000012159 carrier gas Substances 0.000 claims 4
- 238000002485 combustion reaction Methods 0.000 claims 3
- 210000001015 Abdomen Anatomy 0.000 claims 1
- 241000272875 Ardeidae Species 0.000 claims 1
- 210000003608 Feces Anatomy 0.000 claims 1
- 101710028361 MARVELD2 Proteins 0.000 claims 1
- 239000011324 bead Substances 0.000 claims 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims 1
- 239000003245 coal Substances 0.000 claims 1
- 239000002817 coal dust Substances 0.000 claims 1
- 230000000875 corresponding Effects 0.000 claims 1
- 238000001035 drying Methods 0.000 claims 1
- 239000004744 fabric Substances 0.000 claims 1
- 239000000463 material Substances 0.000 claims 1
- 238000003801 milling Methods 0.000 claims 1
- 239000000376 reactant Substances 0.000 claims 1
- 241000273930 Brevoortia tyrannus Species 0.000 description 1
- 239000000969 carrier Substances 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
Description
wandung eingeschoben sind und deren nach außen überstehender Teil als Kühlfahne dient Selbstverständlich wird maa normalerweise stets die gleiche Art von Rauhigkeiten verwenden. Ia dem dargestellten Ausführungsbeispiel sind nur der Einfachheit halber in einem Schnitt zwei verschiedene Arten von Rauhigkeiten dargestellt. Die Zahl der einzelnen Rauhigkeiten zwischen den jeweiligen Düsenreihen wird man entsprechend den Anforderungen an die jeweils erforderliche Turbulenz wählen.wall are inserted and the outwardly protruding part serves as a cooling flag will normally always use the same type of roughness. Ia the one shown Exemplary embodiment are two different types of roughness in one section only for the sake of simplicity shown. The number of individual roughnesses between the respective rows of nozzles is choose according to the requirements of the turbulence required in each case.
Durch Steuerung der Gaszufuhr zu den einzelnen Düsenreihen werden die Teilchen dann jeweils an den nächstunteren Ring, also zunächst zwischen die Düsenreihen 34 bis 36 und 37 bis 39, anschließend zwischen die Düsenreihen 37 bis 39 und 40 bis 42 sowie schließlich zwischen 40 bis 42 und 43 bis 45 weitergegeben. Nach Abschaltung der Gaszufuhr füV die unteiste Düsenreihe 43 bis 45 werden die Teilchen über den Auslaß 29 in einen Bunker abgeführt. Das von Teilchen gereinigte Trägermedium verläßt die Wirbelkammer über den Auslaß 30.By controlling the gas supply to the individual rows of nozzles, the particles are then activated the next ring below, so initially between the rows of nozzles 34 to 36 and 37 to 39, then between the rows of nozzles 37 to 39 and 40 to 42 and finally between 40 to 42 and 43 to 45 passed on. After switching off the gas supply for the bottom row of nozzles 43 to 45, the particles are discharged via the outlet 29 into a bunker. The carrier medium, which has been cleaned of particles, leaves the vortex chamber via outlet 30.
Die Anwendung der beschriebenen Rauhigkeiten ist dabei nicht auf Reaktionsbehälter beschränkt, bei denen die zu behandelnden Teilchen über ein axialesThe application of the roughness described is not limited to reaction vessels which the particles to be treated have an axial
ίο Einströmrohr zugeführt werden. Sie sind vieimehr anwendbar bei allen Einrichtungen, in denen frei schwebend rotierende Teilchenringe erzeugt werden. Die Teilchen selbst können auch auf andere Weise, etwa durch die Düsen selbst oder über einen tangen-ίο the inlet pipe. They are much more Applicable to all facilities in which free-floating, rotating particle rings are generated. The particles themselves can also be produced in other ways, for example through the nozzles themselves or via a tangible
IS tialen Einlauf zugeführt werden.IS tial inlet are fed.
Hierzu 1 Blatt Zeichnungen1 sheet of drawings
Claims (2)
chen sowie mit tangentialen und dem Einlauf Aus diesem Grunde ist nach Mitteln gesucht wor-1. Rotary flow vortex come into contact with fabric and war partners. Does that happen especially between solid or liquid particles? in chemical reactions as they occur, for. B. represents the combustion and gases, consisting of a rotationally symmetrical combustion. If, for example, a moist tric vortex chamber with a lower or wet coal dust is supplied, the coaxial elements projecting into these burn the coal particles in the outer area of the smaller diameter for together with individual rings, but the combustion inside the carrier gas to be supplied or liquid part- io of the rings is quite incomplete,
surfaces as well as with tangentials and the inlet For this reason, means have been sought
sehen Wirbelkammer mit einem im unteren Bereich In der Zeichnung ist ein schematiches Ausfüh-The main patent relates to a Drehströmungswirb- roughness consisting of flat profile pieces, which in ler for mass and heat exchange between solid milled recesses of the vortex chamber jacket such one or liquid particles and gases. The 40 is pushed so that a part of the flat profile pieces of rotary flow vortex protrudes outwards from a rotationally symmetrical cooling vane,
see vortex chamber with a in the lower area In the drawing is a schematic execution
Hilfsgaseinlässen an den Seitenwänden des oberen Die Wirbelkammer 1 weist ein koaxiales Einlaß-shown in this projecting coaxial inlet smaller approximately example according to the invention. F i g shows the diameter to be supplied together with carrier gas. 1 shows a longitudinal section through an escaping solid or liquid particle as well as with elongated vortex chamber and FIG. 2 shows a cross section tiale and the inlet diagonally opposite to the inlet according to the section line H-II.
Auxiliary gas inlets on the side walls of the upper vortex chamber 1 has a coaxial inlet
Family
ID=
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